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Discretized adjoint based aerodynamic design optimization for the hypersonic inward turning inlet
王晓峰 屈峰 付俊杰 王泽宇 刘超宇 白俊强
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 0, (): 0 -0 .  DOI: 10.7527/S1000-6893.2023.28352

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Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics

All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341